Trajectory and maneuvers

• CL_dsp_covCoord — Conversion of type of orbital elements in a covariance matrix
• CL_dsp_kepCovPropa — Keplerian covariance propagation
• CL_ex_eckHech — Eckstein-Hechler propagation model
• CL_ex_eckHechInfos — Informations about Eckstein-Hechler orbit propagation analytical model
• CL_ex_kepler — Keplerian orbit propagation
• CL_ex_lyddane — Orbit propagation using Lyddane model (mean elements = secular)
• CL_ex_lyddaneInfos — Informations about Lyddane orbit propagation analytical model
• CL_ex_lyddaneLp — Orbit propagation using Lyddane model (mean elements = secular + long periods)
• CL_ex_lyddaneMan — Lyddane orbit propagation analytical model with maneuvers
• CL_ex_meanEckHech — Eckstein-Hechler propagation model - mean elements
• CL_ex_meanElem — Mean orbital elements (all analytical models)
• CL_ex_meanLyddane — Lyddane propagation model - mean elements (mean = secular)
• CL_ex_meanLyddaneLp — Lyddane propagation model - mean elements (mean = secular + LP)
• CL_ex_propagate — Orbit propagation (all analytical models)
• CL_ex_secularJ2 — Orbit propagation using "secular J2" model
• CL_man_applyDvKep — Effect of maneuver on orbital elements
• CL_man_consumption — Mass consumed as function of delta-V
• CL_man_dvApsidesLine — Delta V required to change the line of apsides
• CL_man_dvBiElliptic — Bi-elliptic transfer
• CL_man_dvHohmann — Hohmann transfer
• CL_man_dvHohmannG — Generalized Hohmann transfer
• CL_man_dvInc — Inclination maneuver (elliptical orbits)
• CL_man_dvIncRaanCirc — Inclination and RAAN maneuver for circular orbits
• CL_man_dvSma — Change of semi-major axis (elliptical orbits)
• CL_man_lambert — Lambert's problem
• CL_man_thrustDuration — Thrust duration as function of mass consumed